What it approves
Installation of the Mecaer Aviation Group S.p.A. (MAG) VIP Interiors, Part Number 6A6H0000X002001
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
IMPORT SR00223IB Mecaer Aviation Group S.p.A.
Via Per Arona 46 28021 Borgomanero (NO) Italy Part 29 Code of Federal Regulations R00009RD Airbus Helicopters
H160-B
1. Installation of the Mecaer Aviation Group S.p.A. (MAG) VIP Interiors, Part Number 6A6H0000X002001, on the Airbus Helicopters H160-B rotocraft must be in accordance Mecaer Aviation Group S.p.A. Design Data Set, Doc # DDS-2024-039, Issue A, dated September 27, 2024, or later European Union Aviation Safety Agency (EASA) accepted revisions.
1. This Supplemental Type Certificate (STC) is applicable to all serial numbers for these Make-Models.
(See continuation sheet 3) July 7, 2023 October 3, 2024 John Yoo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 4
IMPORT SR00223IB 4
IMPORT SR00223IB Date Issued: October 3, 2024
Description of Type Design Change (continued):
2. Maintenance must be in accordance with Mecaer Aviation Group S.p.A. Owner's Manual (Instructions for Continued Airworthiness), Doc. # 6A6HWNM-2-3, Issue 001 dated April 5, 2024, or later EASA accepted revisions.
3. Operations must be in accordance with Mecaer Aviation Group S.p.A. Rotocraft Flight Manual Supplement, Doc # 6A6HRFM1-3, Revision 0, dated September 23, 2024, or later EASA approved revisions.
Limitations and Conditions (continued)
2. The aircraft must be operated in accordance with the Limitations section of the Rotocraft Flight Manual Supplement referenced in the Description section.
3. The installer must determine whether this design change is compatible with previously approved modifications.
4. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.
Certification Basis:
Based on Title 14 Code of Federal Regulations (CFR) 21.115 and 21.101, and the Federal Aviation Administration (FAA) policy for design changes that are identified as not significant in FAA Order 8110.48, the type certification basis for the modified Airbus Helicopters H160-B is as follows:
a. The type certification basis for the Airbus Helicopters H160-B as shown on Type Certification Data Sheet (TCDS) R00009RD for parts not changed or not affected by the change.
IMPORT SR00223IB Date Issued: October 3, 2024
Certification Basis (continued):
b. The type certification basis for the Airbus Helicopters H160-B for parts changed or affected by the change is TCDS R00009RD in addition to:
• Equivalent Level of Safety (ELOS) findings have been made for title 14 Code of Federal Regulations (CFR) 29.807(c) (Amdt 29-30), Passenger Emergency Exits, documented in ELOS Memorandum ST11792IB-R-29.807, dated March 6, 2024.
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ADs that name this STC · 2
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Airbus Helicopters | H160-B | R00009RD |